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Practice Exam 1

Practice Exam 1
55問 • 1年前
  • Angelo Ortiz
  • 通報

    問題一覧

  • 1

    Where are the localizer and glidescope antennas located?

    Behind the nose radome

  • 2

    What is the wingspan of the A320 without sharklets?

    34.09m

  • 3

    What cargo compartment can handle containers if the aircraft has that option?

    Both FWD and AFT cargo compartment

  • 4

    The ECAM display uses a color code that indicates the importance of the failure or the indication. What color indicates the crew should be aware but not need immediate action?

    Amber

  • 5

    With the aircraft on the ground, engines shutdown and no faults, which page is displayed on the lower ECAM DU (SD)?

    DOOR

  • 6

    What permanent data is displayed on the lower section of the SD

    Temperature, G load, UTC and GW

  • 7

    In normal operation, what displays are receiving information from DMC 1?

    PFD 1, ND 1, E/WD and SD

  • 8

    When does the STATUS page appear automatically?

    Once the crew has cleared all the pages corresponding to the current failure, or when the slats are extended (if failure still exists)

  • 9

    In normal configuration, what sources can supply power to the AC system when the aircraft is on ground?

    GEN 1, GEN 2, external power and APU GEN

  • 10

    Can the generators be connected in parallel?

    No

  • 11

    What’s the purpose of the TR’s?

    To transform and rectify A/C power to D/C power

  • 12

    Which statement is correct?

    GEN 1 and GEN 2 have the highest priority on their own buses (AC bus 1 and 2)

  • 13

    Which of the following units are part of the Flight Management System (FMGS)?

    Two Flight Management Guidance Computers (FMGC), Two Multipurpose Control and Display Unit (MCDU), One Flight Control Unit (FCU), and Two Flight Augmentation Computers (FAC)

  • 14

    How many legs can a flight plan contain?

    200

  • 15

    If AP 2 is engaged, which Flight Management Guidance Computers (FMGC) is master and controls the A/THR?

    #2

  • 16

    What color indicates a secondary flight plan in PLAN mode?

    White

  • 17

    What unit is used for short-term interface?

    Flight Control Unit (FCU)

  • 18

    With the Predictive Windshear (PWS) switch in AUTO, below what height is data displayed on the ND?

    1500 ft RA

  • 19

    How long must the RESET p/b on the Integrated Standby Instrument System (ISIS) be pressed to reset the attitude indication?

    At least 2 seconds

  • 20

    How many GPS receivers are connected to the IR part of the Air Data Inertial Reference Unit (ADIRU)?

    Two independent receivers

  • 21

    If ALL/N is selected on the ATC/TCAS panel, what is the altitude range of intruders that are displayed?

    2700 feet above / 2700 feet below the aircraft

  • 22

    Below what height do the Flight Warning Computer (FWC) generate height announcements?

    2500 feet

  • 23

    What does the message LOW OIL LEVEL means?

    Advisory message regarding APU oil level when aircraft is on the ground and APU not running

  • 24

    When will the APU fire extinguisher discharge automatically?

    On ground only

  • 25

    What methods are available for APU emergency shutdown?

    APU FIRE handle and APU SHUT OFF p/b on the interphone panel under the nose fuselage

  • 26

    Which of the statements is correct?

    Bleed air is cooled by a pre-cooler, using cooling air bleed from the engine fan

  • 27

    The air bleed system supplies the aircraft with high pressure air, and uses it for:

    Air conditioning, engine starting, water system pressurization, wing anti-icing and hydraulic reservoir pressurization

  • 28

    What happens when the pressure and temperature are not sufficient to supply the corresponding engine bleed valve?

    The HP valve opens and the IP stage remains in the same configuration

  • 29

    In the air conditioning system, is temperature regulation of the temperature, is ensured by?

    A zone controller and two pack controllers, or two Air Conditioning System Controllers (ACSC)

  • 30

    When does the hot air valve close automatically?

    When a duct overheat or absence of pneumatic pressure exists

  • 31

    In which part of the air conditioning pack is the hot air expanded?

    In the turbine

  • 32

    In what range can the temperature be regulated with the zone temperature selectors on the overhead panel?

    18-30 deg C

  • 33

    Can the PTU operate and pressurize the Green system without an engine running?

    Yes, by selecting the YELLOW ELEC pump to ON, PTU switch to AUTO, and differential pressure > 500 psi

  • 34

    What is the purpose of the priority valves?

    Priority valves cut off hydraulic power to heavy load users if hydraulic pressure in a system gets low

  • 35

    What is the normal operating hydraulic pressure?

    3000 psi, (2500 psi when powered by RAT)

  • 36

    Which hydraulic systems have a Fire Shutoff Valve?

    Green and Yellow

  • 37

    Side stick control orders are sent to which flight control computer?

    Elevator and Aileron Computer (ELAC) and Spoiler and Elevator Computers (SEC)

  • 38

    Which flight control computer normally operates the ailerons?

    Elevator and Aileron Computer (ELAC) 1

  • 39

    Which spoilers are ground spoilers?

    Spoilers 1-5

  • 40

    What is true regarding the flight controls on an A320?

    They are all electrically controlled and hydraulically activated

  • 41

    Where is the VHF 1 antenna located?

    On top of the fuselage

  • 42

    What is the total length of the A320?

    37.57 m

  • 43

    How are Primary and Secondary failures indicated?

    Primary boxed, Secondary indicated by a star

  • 44

    AC ESS BUS is normally supplied by:

    AC BUS 1

  • 45

    In SRS mode, what speed does the aircraft maintain with 2 engines operative and with 1 engine operative?

    V2 + 10 knots / Highest of V2 or current speed (Maximum V2 + 15 knots)

  • 46

    What is the normal mode for the FMGCs?

    Dual mode

  • 47

    What causes amber XX in the BLEED indication on APU SD page?

    ADIRS 1 or 2 are not available or selected OFF, or the data from the ECB are invalid or not transmitted

  • 48

    When does the APU bleed valve open?

    When N > 95%

  • 49

    What controls and monitors the Pneumatic system?

    Two Bleed Monitoring Computers

  • 50

    What happens when pressure and temperature are not sufficient to supply the corresponding engine bleed valve:

    The HP valve opens and the IP stage remains in the same configuration

  • 51

    The Pressurization system is normally controlled in what way?

    Fully automatic

  • 52

    How are the Pack Flow Control valves controlled during engine start?

    Close automatically

  • 53

    When will the RAT deploy automatically?

    If AC BUS 1 and AC BUS 2 are both lost

  • 54

    Which hydraulic systems have a pump that is driven by an engine?

    Green and yellow

  • 55

    In normal law, what happens if the pilot holds full lateral side stick deflection?

    The bank angle goes to 67° and no further

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    問題一覧

  • 1

    Where are the localizer and glidescope antennas located?

    Behind the nose radome

  • 2

    What is the wingspan of the A320 without sharklets?

    34.09m

  • 3

    What cargo compartment can handle containers if the aircraft has that option?

    Both FWD and AFT cargo compartment

  • 4

    The ECAM display uses a color code that indicates the importance of the failure or the indication. What color indicates the crew should be aware but not need immediate action?

    Amber

  • 5

    With the aircraft on the ground, engines shutdown and no faults, which page is displayed on the lower ECAM DU (SD)?

    DOOR

  • 6

    What permanent data is displayed on the lower section of the SD

    Temperature, G load, UTC and GW

  • 7

    In normal operation, what displays are receiving information from DMC 1?

    PFD 1, ND 1, E/WD and SD

  • 8

    When does the STATUS page appear automatically?

    Once the crew has cleared all the pages corresponding to the current failure, or when the slats are extended (if failure still exists)

  • 9

    In normal configuration, what sources can supply power to the AC system when the aircraft is on ground?

    GEN 1, GEN 2, external power and APU GEN

  • 10

    Can the generators be connected in parallel?

    No

  • 11

    What’s the purpose of the TR’s?

    To transform and rectify A/C power to D/C power

  • 12

    Which statement is correct?

    GEN 1 and GEN 2 have the highest priority on their own buses (AC bus 1 and 2)

  • 13

    Which of the following units are part of the Flight Management System (FMGS)?

    Two Flight Management Guidance Computers (FMGC), Two Multipurpose Control and Display Unit (MCDU), One Flight Control Unit (FCU), and Two Flight Augmentation Computers (FAC)

  • 14

    How many legs can a flight plan contain?

    200

  • 15

    If AP 2 is engaged, which Flight Management Guidance Computers (FMGC) is master and controls the A/THR?

    #2

  • 16

    What color indicates a secondary flight plan in PLAN mode?

    White

  • 17

    What unit is used for short-term interface?

    Flight Control Unit (FCU)

  • 18

    With the Predictive Windshear (PWS) switch in AUTO, below what height is data displayed on the ND?

    1500 ft RA

  • 19

    How long must the RESET p/b on the Integrated Standby Instrument System (ISIS) be pressed to reset the attitude indication?

    At least 2 seconds

  • 20

    How many GPS receivers are connected to the IR part of the Air Data Inertial Reference Unit (ADIRU)?

    Two independent receivers

  • 21

    If ALL/N is selected on the ATC/TCAS panel, what is the altitude range of intruders that are displayed?

    2700 feet above / 2700 feet below the aircraft

  • 22

    Below what height do the Flight Warning Computer (FWC) generate height announcements?

    2500 feet

  • 23

    What does the message LOW OIL LEVEL means?

    Advisory message regarding APU oil level when aircraft is on the ground and APU not running

  • 24

    When will the APU fire extinguisher discharge automatically?

    On ground only

  • 25

    What methods are available for APU emergency shutdown?

    APU FIRE handle and APU SHUT OFF p/b on the interphone panel under the nose fuselage

  • 26

    Which of the statements is correct?

    Bleed air is cooled by a pre-cooler, using cooling air bleed from the engine fan

  • 27

    The air bleed system supplies the aircraft with high pressure air, and uses it for:

    Air conditioning, engine starting, water system pressurization, wing anti-icing and hydraulic reservoir pressurization

  • 28

    What happens when the pressure and temperature are not sufficient to supply the corresponding engine bleed valve?

    The HP valve opens and the IP stage remains in the same configuration

  • 29

    In the air conditioning system, is temperature regulation of the temperature, is ensured by?

    A zone controller and two pack controllers, or two Air Conditioning System Controllers (ACSC)

  • 30

    When does the hot air valve close automatically?

    When a duct overheat or absence of pneumatic pressure exists

  • 31

    In which part of the air conditioning pack is the hot air expanded?

    In the turbine

  • 32

    In what range can the temperature be regulated with the zone temperature selectors on the overhead panel?

    18-30 deg C

  • 33

    Can the PTU operate and pressurize the Green system without an engine running?

    Yes, by selecting the YELLOW ELEC pump to ON, PTU switch to AUTO, and differential pressure > 500 psi

  • 34

    What is the purpose of the priority valves?

    Priority valves cut off hydraulic power to heavy load users if hydraulic pressure in a system gets low

  • 35

    What is the normal operating hydraulic pressure?

    3000 psi, (2500 psi when powered by RAT)

  • 36

    Which hydraulic systems have a Fire Shutoff Valve?

    Green and Yellow

  • 37

    Side stick control orders are sent to which flight control computer?

    Elevator and Aileron Computer (ELAC) and Spoiler and Elevator Computers (SEC)

  • 38

    Which flight control computer normally operates the ailerons?

    Elevator and Aileron Computer (ELAC) 1

  • 39

    Which spoilers are ground spoilers?

    Spoilers 1-5

  • 40

    What is true regarding the flight controls on an A320?

    They are all electrically controlled and hydraulically activated

  • 41

    Where is the VHF 1 antenna located?

    On top of the fuselage

  • 42

    What is the total length of the A320?

    37.57 m

  • 43

    How are Primary and Secondary failures indicated?

    Primary boxed, Secondary indicated by a star

  • 44

    AC ESS BUS is normally supplied by:

    AC BUS 1

  • 45

    In SRS mode, what speed does the aircraft maintain with 2 engines operative and with 1 engine operative?

    V2 + 10 knots / Highest of V2 or current speed (Maximum V2 + 15 knots)

  • 46

    What is the normal mode for the FMGCs?

    Dual mode

  • 47

    What causes amber XX in the BLEED indication on APU SD page?

    ADIRS 1 or 2 are not available or selected OFF, or the data from the ECB are invalid or not transmitted

  • 48

    When does the APU bleed valve open?

    When N > 95%

  • 49

    What controls and monitors the Pneumatic system?

    Two Bleed Monitoring Computers

  • 50

    What happens when pressure and temperature are not sufficient to supply the corresponding engine bleed valve:

    The HP valve opens and the IP stage remains in the same configuration

  • 51

    The Pressurization system is normally controlled in what way?

    Fully automatic

  • 52

    How are the Pack Flow Control valves controlled during engine start?

    Close automatically

  • 53

    When will the RAT deploy automatically?

    If AC BUS 1 and AC BUS 2 are both lost

  • 54

    Which hydraulic systems have a pump that is driven by an engine?

    Green and yellow

  • 55

    In normal law, what happens if the pilot holds full lateral side stick deflection?

    The bank angle goes to 67° and no further